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TudatPy version 1.0 has been released 🥳 For more information, see our migration guide! As always, you can post any questions or feedback in our Github Discussion forum
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  • Getting Started
  • Examples
  • User Guide
  • API Reference
  • About
  • Getting Started
  • Examples
  • User Guide
  • API Reference
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Section Navigation

Tudatpy example categories

  • Propagation
    • Keplerian satellite orbit
    • Perturbed satellite orbit
    • Linear sensitivity analysis using variational equations
    • Solar System Propagation using Multi-Body Dynamics
    • Thrust between the Earth and the Moon
    • JUICE Flybys of Jovian Moons
    • Setup a Panelled Radiation Pressure Model
    • Re-entry trajectory using custom aerodynamic guidance
    • Two-stage rocket ascent
    • Separation of satellites via differential drag
    • Basic thrust model for satellite engines
    • Propagation of coupled translational-rotational dynamics
    • Impact Manifolds of Lagrange Point Orbits in CR3BP(-Polyhedron)
  • Estimation
    • Covariance Analysis with DELFI-C3
    • Covariance Propagation Using Starlink-32101
    • Parameter Estimation with DELFI-C3
    • Simulation and Estimation Using Different Dynamical Models
    • Generating Visibility Plots with Tudat
    • Automatically Download Mission data
    • Initial State Estimation Using NOE-5 Ephemeris
    • Retrieving Observations From the Minor Planet Centre
    • Initial state estimation From Real MPC Observations
    • Improved state estimation with MPC
    • Loading and Using Tracking Observations
    • Kosmos 482 Re-entry
    • MRO - Comparing Doppler and Range Measurements from TNF Files to Simulated Observables
    • GRAIL - Comparing Doppler measurements from ODF files to simulated observables
    • GRAIL - Estimating the spacecraft trajectory from ODF Doppler measurements
    • GRAIL - Fitting various models of the GRAIL spacecraft’s dynamics to the reference spice trajectory
  • Mission Design
    • Multiple Gravity Assist trajectories
    • Earth-Mars transfer window design using Porkchop Plots
    • Earth-Mars transfer window design using Porkchop Plots
    • Hodographic-shaping MGA transfer optimization with PyGMO
    • Cassini 1 (MGA transfer) optimization with PyGMO
  • Optimization using PyGMO
    • Himmelblau minimization with PyGMO
    • Asteroid Orbit Optimization
      • Asteroid orbit optimization with PyGMO - Custom Environment
      • Asteroid orbit optimization with PyGMO - Design Space Exploration
      • Asteroid orbit optimization with PyGMO - Optimization
  • Examples

Examples#

The examples below will help you get started in exploring the diverse capabilities of Tudat!

Tudatpy example categories

Propagation
Estimation
Mission Design
Optimization using PyGMO

Github Repository

The same examples shown above available on Github, both as Jupyter notebooks and regular .py files, in the tudatpy-examples repository.

Go to the repository

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Propagation

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